The multi-rotor type unmanned aerial vehicle includes: a main body including the battery module and the control module; a plurality of frames connected to a side surface of the main body and extending therefrom; a first motor connected to a distal end of each of the frames; and a drive unit connected to the first motor, wherein the drive unit includes a rotary frame and a stationary frame each having a circular shape and connected to each other in the form of a gyroscope, a second motor supported at the center of the rotatable frame, and a propeller connected to the second motor, and a vector of thrust generated by rotation of the propeller is variable according to rotation of the first and second motors.


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    Titel :

    MULTIROTOR TYPE UNMANNED AERIAL VEHICLE AVAILABLE FOR ADJUSTING DIRECTION OF THRUST


    Beteiligte:
    AHN HYO SUNG (Autor:in) / CHOI YOUNG CHEOL (Autor:in) / KANG SUNG MO (Autor:in) / SON JI HWAN (Autor:in) / LEE BYUNG HUN (Autor:in) / KO GWI HAN (Autor:in)

    Erscheinungsdatum :

    10.11.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge




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